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  • © 2006

Interplanetary Mission Analysis and Design

Authors:

  • The most up-to-date book focusing entirely on interplanetary mission design for a wide range of space projects
  • Describes the very latest and most efficient mission design techniques with details of their practical applications
  • Covers a wide range of interplanetary mission design problems with case studies of their use in actual European space mission design scenarios
  • Includes relevant mathematical methods and algorithms as they are required in a problem solving context
  • Includes supplementary material: sn.pub/extras

Part of the book series: Springer Praxis Books (PRAXIS)

Part of the book sub series: Astronautical Engineering (ASTROENG)

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Table of contents (5 chapters)

  1. Front Matter

    Pages i-xxxvi
  2. Spacecraft propulsion

    Pages 73-87
  3. Optimisation

    Pages 89-134
  4. Special techniques

    Pages 135-333
  5. Missions to the planets

    Pages 335-427
  6. Back Matter

    Pages 429-484

About this book

The book describes current mission analysis and design techniques that may be applied to a very wide range of interplanetary missions from those targeting the inner planets to those destined for the outer planets and Solar System escape trajectories. The early chapters comprise an introduction and a description of the fundamentals of interplanetary missions, aspects of leaving Earth and planet orbit selection and insertion. A discussion of various propulsion systems for interplanetary transfer is followed by a detailed overview of transfer techniques, including the principles of gravity assist and a range of applications of this technique, low-thrust transfers in combination with gravity assist and for planetary escape and capture and the utilisation of multi-body gravity perturbations. The final chapter deals with various optimisation methods for interplanetary missions.

The dynamics of the problems are analysed and algorithms that may be used to solve the problems are presented. Practical difficulties that may be encountered are also discussed. The mission design options are considered in the context of spacecraft types, ranging from high thrust, nuclear thermal rockets to low thrust ion propulsion systems. A series of specific examples are described in detail in the appendices, covering ‘end-to-end’ mission design for some topical space mission scenarios.

Authors and Affiliations

  • EADS Astrium, Stevenage, Hertfordshire, UK

    Stephen Kemble

Bibliographic Information

Buy it now

Buying options

eBook USD 169.00
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever

Tax calculation will be finalised at checkout

Other ways to access